High burning rate propellant formulation used in broad temperature range

Tuijin Jishu/Journal of Propulsion Technology

Volumn 22, Issue 2, 2001, Pages 162-164

  Lu, Guo Lin ^a   Yin, Rui Kang ^a   Liu, Yue ^a  

^a Hubei Red Star Chemical Research Institute   (China)

Author keywords

High burning rate propellant; High temperature propellant; Hydroxy terminated polybutadience propellant; Performance of low temperature mechanics

Indexed keywords

AMMONIUM COMPOUNDS; COMBUSTION; HIGH TEMPERATURE EFFECTS; TENSILE STRENGTH;

HYDROXY TERMINATED POLYBUTADIENE (HTPB) PROPELLANT; ELONGATION; HIGH BURNING RATE PROPELLANT; HIGH TEMPERATURE PROPELLANT; HYDROXY TERMINATED POLYBUTADIENCE; MECHANICAL PROPERTIES; PROPELLANT FORMULATION;

SOLID PROPELLANTS; PROPELLANTS;

EID: 0035297492     PISSN: 10014055     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (4)

1. MeGee, L R, et al. Development of HTPB propellants for the SRAM motor[R]. AIAA78-173.